METEOSAT 6 AKM, 23118

Orbit data source: Space-Track

METEOSAT 6 AKM, 23118 is space debris in GEO originally from a launch on Sat, 20 Nov 1993 UTC launched from the French Guiana (FRGUI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
23118, 1993-073E
Orbit
GEO
Country
Flag of ESAESA
Related business
Manufacturer
SEP
Mission
Spacecraft
Bus & Motor
MAGE, Unknown motor
Mass
364 kg wet, ~71 kg dry
Launch date (UTC)
1993-11-20 (33 years ago)
Launch vehicle
Unknown
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 0.6 m
Radar Cross Section
0.910 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 4 weeks ago

TLE from 4 weeks ago
0 METEOSAT 6 AKM
1 23118U 93073E   26241.17198284 -.00000290  00000-0  00000-0 0  9994
2 23118  14.1714 346.5469 0066602 112.2438 258.0923  0.99995015 47921
Epoch: 2026-08-29T04:07Z
TLE epoch observation values (Epoch: 2026-08-29T04:07:39.317Z)
Latitude
2.32528°
Longitude
-43.46432°
Altitude
35,924.965 km
Speed
3.067 km/s
True Right ascension
23h 43m 20s
True Declination
2° 19' 23"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,146.687 km
Perigee altitude
35,583.987 km
Semi-major axis
42,243.474 km
Eccentricity
0.00666
Inclination
14.1714°
RAAN
346.5469°
Arg. of periapsis
112.2438°
True anomaly
257.34682°
Mean anomaly
258.0923°
Eccentric anomaly
257.71943°
Mean motion
0.24998 °/min
Orbital period
1,440.12 mins
BSTAR
0
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